US20170307082A1 - Hybrid piston pin and manufacturing method thereof - Google Patents

Hybrid piston pin and manufacturing method thereof Download PDF

Info

Publication number
US20170307082A1
US20170307082A1 US15/352,463 US201615352463A US2017307082A1 US 20170307082 A1 US20170307082 A1 US 20170307082A1 US 201615352463 A US201615352463 A US 201615352463A US 2017307082 A1 US2017307082 A1 US 2017307082A1
Authority
US
United States
Prior art keywords
prepreg
reinforcement layer
reinforced fibers
cylindrical pin
pin
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US15/352,463
Inventor
Sang Yoon Park
Jeong Min CHO
Chi Hoon Choi
Jong Dae Lim
Hee Sam Kang
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hyundai Motor Co
Original Assignee
Hyundai Motor Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hyundai Motor Co filed Critical Hyundai Motor Co
Publication of US20170307082A1 publication Critical patent/US20170307082A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J1/00Pistons; Trunk pistons; Plungers
    • F16J1/10Connection to driving members
    • F16J1/14Connection to driving members with connecting-rods, i.e. pivotal connections
    • F16J1/16Connection to driving members with connecting-rods, i.e. pivotal connections with gudgeon-pin; Gudgeon-pins
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J7/00Piston-rods
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C35/00Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C53/00Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/02Bending or folding
    • B29C53/04Bending or folding of plates or sheets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C63/00Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor
    • B29C63/0065Heat treatment
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C63/00Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor
    • B29C63/18Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor using tubular layers or sheathings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/48Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721Fibre-reinforced materials
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/74Joining plastics material to non-plastics material
    • B29C66/742Joining plastics material to non-plastics material to metals or their alloys
    • B29C66/7428Transition metals or their alloys
    • B29C66/74283Iron or alloys of iron, e.g. steel
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B1/00Layered products having a general shape other than plane
    • B32B1/08Tubular products
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/04Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/14Layered products comprising a layer of metal next to a fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/18Layered products comprising a layer of metal comprising iron or steel
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/06Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B27/08Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/12Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/12Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer characterised by the relative arrangement of fibres or filaments of different layers, e.g. the fibres or filaments being parallel or perpendicular to each other
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/26Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/02Physical, chemical or physicochemical properties
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04Interconnection of layers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04Interconnection of layers
    • B32B7/12Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F3/00Pistons 
    • F02F3/0015Multi-part pistons
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C63/00Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor
    • B29C63/02Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor using sheet or web-like material
    • B29C63/04Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor using sheet or web-like material by folding, winding, bending or the like
    • B29C63/08Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor using sheet or web-like material by folding, winding, bending or the like by winding helically
    • B29C63/10Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor using sheet or web-like material by folding, winding, bending or the like by winding helically around tubular articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/08Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
    • B29K2105/0872Prepregs
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2307/00Use of elements other than metals as reinforcement
    • B29K2307/04Carbon
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/748Machines or parts thereof not otherwise provided for
    • B29L2031/7494Pistons
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2250/00Layers arrangement
    • B32B2250/044 layers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/02Composition of the impregnated, bonded or embedded layer
    • B32B2260/021Fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/02Composition of the impregnated, bonded or embedded layer
    • B32B2260/021Fibrous or filamentary layer
    • B32B2260/023Two or more layers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/04Impregnation, embedding, or binder material
    • B32B2260/046Synthetic resin
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/02Synthetic macromolecular fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10Inorganic fibres
    • B32B2262/106Carbon fibres, e.g. graphite fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/50Properties of the layers or laminate having particular mechanical properties
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/50Properties of the layers or laminate having particular mechanical properties
    • B32B2307/51Elastic
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/50Properties of the layers or laminate having particular mechanical properties
    • B32B2307/546Flexural strength; Flexion stiffness
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/70Other properties
    • B32B2307/718Weight, e.g. weight per square meter
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/70Other properties
    • B32B2307/732Dimensional properties
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/70Other properties
    • B32B2307/752Corrosion inhibitor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2597/00Tubular articles, e.g. hoses, pipes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2605/00Vehicles
    • B32B2605/08Cars
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2605/00Vehicles
    • B32B2605/12Ships
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2605/00Vehicles
    • B32B2605/18Aircraft

Definitions

  • the present invention provides a hybrid piston pin and a manufacturing method thereof and, more particularly, to a hybrid piston pin, in which the interior surface of a cylindrical pin formed of steel is sequentially reinforced with a reinforcement layer formed of reinforced fibers having high elasticity and a reinforcement layer formed of reinforced fibers having relatively low elasticity, to provide flexural strength in a circular arrangement and flexural strength in a length direction and to achieve weight reduction.
  • a piston pin formed of steel, manufactured using conventional SMC415 steel, is heavy and does not contribute to improvement in fuel efficiency when the piston pin is applied to a vehicle. Further, the piston pin does not satisfy flexural strength in a hoop direction and flexural strength in a length direction that is required for general piston pins. Therefore, manufacture of a piston pin to substitute a conventional piston pin is required. Accordingly, a hybrid piston pin formed of a composite that includes carbon fibers having a light weight and high strength is proposed.
  • the present invention provides a hybrid piston pin, in which the interior surface of a cylindrical pin formed of steel is sequentially reinforced with a reinforcement layer formed of reinforced fibers having a greater elasticity and a reinforcement layer formed of reinforced fibers having relatively lower elasticity to have improved flexural strength in a circular arrangement and flexural strength in a length direction and to reduce the overall weight.
  • a hybrid piston pin may include a cylindrical pin formed of steel, a first reinforcement layer formed of a composite that includes reinforced fibers and a resin having a cylindrical shape with a substantially uniform thickness and coupled to the interior surface of the cylindrical pin and a second reinforcement layer formed of a composite that includes reinforced fibers having an elasticity less than the reinforced fibers of the first reinforcement layer and a resin having a cylindrical shape with a substantially uniform thickness and coupled to the interior surface of the first reinforcement layer.
  • the reinforced fibers of the first reinforcement layer and the second reinforcement layer may be carbon fibers.
  • the reinforced fibers of the first reinforcement layer may be pitch-based carbon fibers and the reinforced fibers of the second reinforcement layer may be PAN-based carbon fibers.
  • a thickness ratio of the cylindrical pin to the first reinforcement layer may be about 1:3 ⁇ 1:6.
  • a thickness ratio of the cylindrical pin to the second reinforcement layer may be about 1:4 ⁇ 1:7.
  • the second reinforcement layer may include a first composite layer formed of reinforced fibers and a resin and may be disposed parallel with the length direction of the cylindrical pin.
  • a second composite layer may be formed of reinforced fibers and a resin and may be disposed perpendicular to the length direction of the cylindrical pin.
  • the hybrid piston pin may further include an adhesive film disposed between the cylindrical pin and the first reinforcement layer to couple the first reinforcement layer to the cylindrical pin.
  • a manufacturing method of hybrid piston pin may include stacking a first prepreg including reinforced fibers and a resin and a second prepreg including reinforced fibers that has an elasticity less than the reinforced fibers of the first prepreg and a resin, rolling the first prepreg and the second prepreg to form an exterior surface with the first prepreg, integrally molding the rolled first prepreg and second prepreg in an oven, and attaching the molded first prepreg and second prepreg to the interior surface of a cylindrical pin formed of steel.
  • the reinforced fibers of the first prepreg and the second prepreg may be carbon fibers, the reinforced fibers of the first prepreg may be pitch-based carbon fibers, and the reinforced fibers of the second prepreg may be PAN-based carbon fibers.
  • a thickness ratio of the cylindrical pin to the first prepreg may be about 1:3 ⁇ 1:6.
  • a thickness ratio of the cylindrical pin to the second prepreg may be about 1:4 ⁇ 1:7.
  • the manufacturing method may further include wrapping the exterior surface of the rolled first prepreg and second prepreg with an anti-resistant film, after rolling.
  • FIG. 1 is an exemplary perspective view illustrating a hybrid piston pin in accordance with an exemplary embodiment of the present invention
  • FIG. 2 is an exemplary cross-sectional view of the hybrid piston pin in accordance with an exemplary embodiment of the present invention
  • FIG. 3 is an exemplary view illustrating when a first prepreg and a second prepreg are rolled and the exterior surface of the first prepreg is wrapped with a film in accordance with an exemplary embodiment of the present invention.
  • FIG. 4 is an exemplary view illustrating when the first prepreg and the second prepreg are integrally molded in an oven in accordance with an exemplary embodiment of the present invention.
  • a layer is “on” another layer or substrate, the layer may be directly on another layer or substrate or a third layer may be disposed therebetween.
  • the term “about” is understood as within a range of normal tolerance in the art, for example within 2 standard deviations of the mean. “About” can be understood as within 10%, 9%, 8%, 7%, 6%, 5%, 4%, 3%, 2%, 1%, 0.5%, 0.1%, 0.05%, or 0.01% of the stated value. Unless otherwise clear from the context, all numerical values provided herein are modified by the term “about.”
  • vehicle or “vehicular” or other similar term as used herein is inclusive of motor vehicle in general such as passenger automobiles including sports utility vehicles (SUV), buses, trucks, various commercial vehicles, watercraft including a variety of boats, ships, aircraft, and the like and includes hybrid vehicles, electric vehicles, combustion, plug-in hybrid electric vehicles, hydrogen-powered vehicles and other alternative fuel vehicles (e.g. fuels derived from resources other than petroleum).
  • motor vehicle in general such as passenger automobiles including sports utility vehicles (SUV), buses, trucks, various commercial vehicles, watercraft including a variety of boats, ships, aircraft, and the like and includes hybrid vehicles, electric vehicles, combustion, plug-in hybrid electric vehicles, hydrogen-powered vehicles and other alternative fuel vehicles (e.g. fuels derived from resources other than petroleum).
  • SUV sports utility vehicles
  • plug-in hybrid electric vehicles e.g. fuels derived from resources other than petroleum
  • a hybrid piston pin in accordance with the present invention may include a cylindrical pin 100 formed of steel, a first reinforcement layer 200 formed of a composite that includes reinforced fibers and a resin, having a cylindrical shape with a substantially uniform thickness and coupled to the interior surface of the cylindrical pin 100 and a second reinforcement layer 300 formed of a composite that includes reinforced fibers having an elasticity less than the reinforced fibers of the first reinforcement layer 200 and a resin, having a cylindrical shape with a uniform thickness and coupled to the interior surface of the first reinforcement layer 200 .
  • a conventional piston pin is formed of SMC415 steel. Therefore, the conventional piston has a thickness of about 4.3 mm and a weight of about 79 g.
  • the cylindrical pin 100 of the present invention may be formed of steel and in particular, may be formed of SMC415 steel. As will be described, reinforced materials may be coupled to the interior surface of the cylindrical pin 100 and the thickness of the cylindrical pin 100 may be reduced up to about 0.5-1.2 mm.
  • the thickness of the cylindrical pin 100 is less than about 0.5 mm, flexural strength in a circular arrangement and flexural strength in a length direction may be diminished and thus, the cross-section of the cylindrical pin 100 may be deformed into an oval shape and the minimal thickness of the cylindrical pin 100 may not satisfy the required size tolerance.
  • the thickness of the cylindrical pin 100 exceeds about 1.2 mm, the hybrid piston pin of the present invention does not exhibit weight reduction effects as compared to the conventional piston pin formed of steel. Therefore, the thickness of the cylindrical pin 100 may be limited within the range of about 0.5-1.2 mm.
  • the cylindrical pin 100 formed of steel may be disposed at the exterior most portion of the hybrid piston pin, may prevent thermal damage and may protect the reinforced materials.
  • the exterior diameter of the cylindrical pin 100 may be within the range of about 7-9 mm.
  • the first reinforcement layer 200 may be rolled to have a cylindrical shape with a substantially uniform thickness and may be coupled to the interior surface of the cylindrical pin 100 .
  • the first reinforcement layer 200 may be formed of a composite that includes reinforced fibers and a resin.
  • the first reinforcement layer 200 may be formed of a prepreg formed by pre-impregnating fibers with a resin.
  • the second reinforcement layer 300 may be rolled to have a cylindrical shape with a substantially uniform thickness and may be coupled to the interior surface of the first reinforcement layer 200 .
  • the second reinforcement layer 300 may be formed of a composite and may include reinforced fibers and a resin.
  • the second reinforcement layer 300 may be formed of a prepreg by pre-impregnating fibers with a resin.
  • the reinforced fibers of the second reinforcement layer 300 may include a reduced elasticity as compared with the reinforced fibers of the first reinforcement layer 200 .
  • elasticity of the reinforced fibers of the second reinforcement layer 300 may be about one third or less that of the reinforced fibers of the first reinforcement layer 200 .
  • the reinforced fibers that form the first reinforcement layer 200 and the second reinforcement layer 300 may be carbon fibers
  • the reinforced fibers of the first reinforcement layer 200 may be pitch-based carbon fibers
  • the reinforced fibers of the second reinforcement layer 300 may be PAN-based carbon fibers.
  • Pitch-based carbon fibers may have an elastic modulus of about 640 GPa or greater and may generally have an increased carbon content and an increased elasticity. Accordingly, the flexural strength and material strength of the hybrid piston pin in the circular arrangement when pitch-based carbon fibers may be coupled to the interior surface of the cylindrical pin 100 formed of steel. For example, the generation of deformation of the cylindrical pin 100 into an oval shape and bending deformation of the cylindrical pin 100 may be suppressed due to an applied load.
  • PAN-based carbon fibers which have an elastic modulus of about 240 GPa or greater, may generally have an increased compressive strength. Further, the PAN-based carbon fibers may support the first reinforcement layer 200 and may withstand load when disposed at the interior most portion of the hybrid piston pin and the flexural strength of the hybrid piston pin in the circular arrangement may be increased. Accordingly, generation of deformation of the cylindrical pin 100 into an oval shape may be suppressed. PAN-based carbon fibers are relatively inexpensive and may reduce the cost. Further, as exemplarily shown in FIG. 2 , the second reinforcement layer 300 may include a first composite layer 310 formed of reinforced fibers and a resin and may be disposed in parallel with the length direction of the cylindrical pin 100 . Further, a second composite layer 320 formed of reinforced fibers and a resin and may be disposed perpendicular to the length direction of the cylindrical pin 100 .
  • the reinforced fibers of the second reinforcement layer 300 are not limited to being disposed in one direction, for example, the reinforced fibers of the first composite layer 310 coupled to the interior surface of the first reinforcement layer 200 may be disposed in a direction parallel with the cylindrical pin 100 and the reinforced fibers of the second composite layer 320 coupled to the interior surface of the first composite layer 310 may be disposed in a direction perpendicular to the cylindrical pin 100 . Accordingly, the stiffness of the hybrid piston pin may be improved and may withstand load applied in the width direction of the hybrid piston pin as well as load applied in the length direction of the hybrid piston pin.
  • first reinforcement layer 200 and the second reinforcement layer 300 may be integrally molded to increase a coupling degree of the first reinforcement layer 200 and the second reinforcement layer 300 .
  • an adhesive film may be coupled to the exterior surface of the first reinforcement layer 200 to couple the first reinforcement layer 200 to the cylindrical pin 100 via the adhesive film.
  • the reinforced fibers of the first reinforcement layer 200 are carbon fibers
  • potential corrosion may occur due to a potential difference between the carbon fibers and the cylindrical pin 100 formed of steel.
  • the adhesive film may interrupt direct contact between the carbon fibers and the cylindrical pin 100 and may prevent potential corrosion to improve the durability of the hybrid piston pin.
  • the hybrid piston pin may have a weight of about 25-42 g and may achieve weight reduction by 46% or greater compared to conventional piston pins. Accordingly, when the hybrid piston pin of the present invention is applied to a vehicle, fuel efficiency of the vehicle may be improved by about 0.7-1.2%. Further, the hybrid piston pin of the present invention may have flexural strength in a circular arrangement of 57 MPa or greater and flexural strength in the length direction of 53 MPa and may satisfy desired material properties.
  • a hybrid piston pin in Test example 1 includes a first reinforcement layer 200 formed of pitch-based carbon fibers having relatively high elasticity and a second reinforcement layer 300 formed of PAN-based carbon fibers.
  • the PAN-based carbon fiber has a relatively low elasticity and improved compressive strength and has flexural strength in a circular arrangement and flexural strength in the length direction, which are equal to or greater than those of a piston pin in Comparative example 1 that include a reinforcement layer formed of pitch-based carbon fibers.
  • the hybrid piston pin in Test example 1 has improved flexural strength in the circular arrangement than a piston pin in Comparative example 2 and includes a reinforcement layer formed of PAN-based carbon fibers.
  • the piston pin in Comparative example 2 has a flexural modulus less than the hybrid piston pin in Test example 1.
  • the hybrid piston pin in Test example 1 has a greater flexural strength in the circular arrangement than a piston pin in Comparative example 3 that includes an exterior reinforcement layer formed of PAN-based carbon fibers and an interior reinforcement layer formed of pitch-based carbon fibers.
  • Thickness ratio of cylindrical of cylindrical Flexural Flexural Flexural Flexural pin to first pin to second strength in strength in modulus modulus reinforcement reinforcement circular length in circular in length layer layer arrangement direction arrangement direction Test example 1:3 1:7 57 MPa 74 MPa 129 GPa 64 GPa 2 Test example 1:4 1:6 65 MPa 67 MPa 119 GPa 73 GPa 3 Test example 1:5 1:5 71 MPa 59 MPa 109 GPa 81 GPa 4 Test example 1:6 1:4 75 MPa 53 MPa 102 GPa 85 GPa 5 Comparative 1:2 1:7 41 MPa 70 MPa 131 GPa 44 GPa example 4 Comparative 1:7 1:4 63 MPa 50 MPa 122 GPa 72 GPa example 5 Comparative 1:6 1:3 72 MPa 48 MPa 102 GPa 82 GPa example 6 Comparative 1:3 1:8 49 MPa 75 MPa 136 GPa 54 GPa example 7
  • a hybrid piston pin in Comparative example 4 has a thickness ratio of a cylindrical pin 100 to a first reinforcement layer 200 of less than 1:3 and has diminished flexural strength in the circular arrangement.
  • a hybrid piston pin in Comparative example 5 has a thickness ratio of a cylindrical pin 100 to a first reinforcement layer 200 which exceeds a ratio of about 1:6 an has diminished flexural strength in the length direction.
  • a hybrid piston pin in Comparative example 6 has a thickness ratio of a cylindrical pin 100 to a second reinforcement layer 300 of less a ratio of about 1:4 and has reduced flexural strength in the length direction.
  • a hybrid piston pin in Comparative example 7 has a thickness ratio of a cylindrical pin 100 to a second reinforcement layer 300 which exceeds a ratio of about 1:7 and has a reduced flexural strength in the circular arrangement.
  • a manufacturing method of a hybrid piston pin in accordance with the present invention includes stacking a first prepreg 10 that includes reinforced fibers and a resin and a second prepreg 20 that include reinforced fibers with a reduced elasticity as compared to the reinforced fibers of the first prepreg 10 .
  • a resin may be formed by rolling the first prepreg 10 and the second prepreg 20 to form the exterior surface of the first prepreg 10 .
  • the rolled first prepreg 10 and second prepreg 20 is integrally molded in an oven.
  • the molded first prepreg 10 and second prepreg 20 is attached to the interior surface of a cylindrical pin 100 formed of steel.
  • the first prepreg 10 and the second prepreg 20 may be sequentially stacked in the upward direction and may then be rolled.
  • the stacked first prepreg 10 and second prepreg 20 may be rolled to form the exterior surface of the first prepreg 10 having relatively high elasticity.
  • the exterior surface of the rolled first prepreg 10 and second prepreg 20 may be wrapped with a film 30 .
  • a heat shrinkable tape having heat resistance may be employed.
  • the first prepreg 10 and second prepreg 20 wrapped with the film 30 , may be placed into the oven and may be integrally molded.
  • the film 30 may shrink during heat exposure during molding within the oven and mesopores may be removed from the first prepreg 10 and second prepreg 20 .
  • the film 30 may be removed and the molded first prepreg 10 and second prepreg 20 may be coupled to the interior surface of the cylindrical pin 100 .
  • processing may include cutting, surface grinding, etc., may be performed to complete manufacture of the hybrid piston pin.
  • the reinforced fibers of the first prepreg 10 and the second prepreg 20 may be carbon fibers.
  • the carbon fibers of the first prepreg 10 may be pitch-based carbon fibers
  • the carbon fibers of the second prepreg 20 may be PAN-based carbon fibers and elasticity of the first prepreg 10 may be greater than elasticity of the second prepreg 20 .
  • the stacked first prepreg 10 and second prepreg 20 may be coupled to the interior surface of the cylindrical pin 100 .
  • a thickness ratio of the cylindrical pin 100 to the first prepreg 10 may be about 1:3 ⁇ 1:6. Further, a thickness ratio of the cylindrical pin 100 to the second prepreg 20 to may be about 1:4 ⁇ 1:7.
  • a hybrid piston pin in accordance with the present invention may be manufactured by sequentially stacking a reinforcement layer that includes reinforced fibers having high elasticity and a reinforcement layer that includes reinforced fibers having relatively low elasticity on the interior surface of a cylindrical pin formed of steel. Accordingly, the flexural strength in a circular arrangement may be increased and flexural strength in a length direction may be increased and a weight reduction by about 47 ⁇ 67%, as compared to a conventional piston pin formed of steel may be achieved. Further, due to weight reduction, when the hybrid piston pin is applied to a vehicle fuel efficiency of the vehicle may be improved by about 0.7 ⁇ 1.2% and costs may be reduced reduction.

Abstract

A hybrid piston pin and a manufacturing method thereof are provided. The hybrid piston pin includes a cylindrical pin formed of steel, a first reinforcement layer that is formed of a composite that includes reinforced fibers and a resin, having a cylindrical shape with a uniform thickness, and coupled to the interior surface of the cylindrical pin. A second reinforcement layer is formed of a composite that includes reinforced fibers having an elasticity that is less than the reinforced fibers of the first reinforcement layer. Further, a resin having a cylindrical shape with a uniform thickness is coupled to the interior surface of the first reinforcement layer.

Description

    CROSS-REFERENCE TO RELATED APPLICATION
  • This application claims the priority benefit of Korean Patent Application No. 10-2016-0049898, filed on Apr. 25, 2016, in the Korean Intellectual Property Office, the disclosure of which is incorporated herein by reference.
  • BACKGROUND 1. Field of the Invention
  • The present invention provides a hybrid piston pin and a manufacturing method thereof and, more particularly, to a hybrid piston pin, in which the interior surface of a cylindrical pin formed of steel is sequentially reinforced with a reinforcement layer formed of reinforced fibers having high elasticity and a reinforcement layer formed of reinforced fibers having relatively low elasticity, to provide flexural strength in a circular arrangement and flexural strength in a length direction and to achieve weight reduction.
  • 2. Description of the Related Art
  • A piston pin formed of steel, manufactured using conventional SMC415 steel, is heavy and does not contribute to improvement in fuel efficiency when the piston pin is applied to a vehicle. Further, the piston pin does not satisfy flexural strength in a hoop direction and flexural strength in a length direction that is required for general piston pins. Therefore, manufacture of a piston pin to substitute a conventional piston pin is required. Accordingly, a hybrid piston pin formed of a composite that includes carbon fibers having a light weight and high strength is proposed.
  • The above information disclosed in this section is merely for enhancement of understanding of the background of the invention and therefore it may contain information that does not form the prior art that is already known in this country to a person of ordinary skill in the art.
  • SUMMARY
  • The present invention provides a hybrid piston pin, in which the interior surface of a cylindrical pin formed of steel is sequentially reinforced with a reinforcement layer formed of reinforced fibers having a greater elasticity and a reinforcement layer formed of reinforced fibers having relatively lower elasticity to have improved flexural strength in a circular arrangement and flexural strength in a length direction and to reduce the overall weight.
  • In accordance with an aspect of the present invention, a hybrid piston pin may include a cylindrical pin formed of steel, a first reinforcement layer formed of a composite that includes reinforced fibers and a resin having a cylindrical shape with a substantially uniform thickness and coupled to the interior surface of the cylindrical pin and a second reinforcement layer formed of a composite that includes reinforced fibers having an elasticity less than the reinforced fibers of the first reinforcement layer and a resin having a cylindrical shape with a substantially uniform thickness and coupled to the interior surface of the first reinforcement layer.
  • The reinforced fibers of the first reinforcement layer and the second reinforcement layer may be carbon fibers. The reinforced fibers of the first reinforcement layer may be pitch-based carbon fibers and the reinforced fibers of the second reinforcement layer may be PAN-based carbon fibers. A thickness ratio of the cylindrical pin to the first reinforcement layer may be about 1:3˜1:6. A thickness ratio of the cylindrical pin to the second reinforcement layer may be about 1:4˜1:7.
  • The second reinforcement layer may include a first composite layer formed of reinforced fibers and a resin and may be disposed parallel with the length direction of the cylindrical pin. A second composite layer may be formed of reinforced fibers and a resin and may be disposed perpendicular to the length direction of the cylindrical pin. The hybrid piston pin may further include an adhesive film disposed between the cylindrical pin and the first reinforcement layer to couple the first reinforcement layer to the cylindrical pin.
  • In accordance with another aspect of the present invention, a manufacturing method of hybrid piston pin may include stacking a first prepreg including reinforced fibers and a resin and a second prepreg including reinforced fibers that has an elasticity less than the reinforced fibers of the first prepreg and a resin, rolling the first prepreg and the second prepreg to form an exterior surface with the first prepreg, integrally molding the rolled first prepreg and second prepreg in an oven, and attaching the molded first prepreg and second prepreg to the interior surface of a cylindrical pin formed of steel.
  • In some exemplary embodiments, in stacking of the first prepreg and the second prepreg, the reinforced fibers of the first prepreg and the second prepreg may be carbon fibers, the reinforced fibers of the first prepreg may be pitch-based carbon fibers, and the reinforced fibers of the second prepreg may be PAN-based carbon fibers. A thickness ratio of the cylindrical pin to the first prepreg may be about 1:3˜1:6. A thickness ratio of the cylindrical pin to the second prepreg may be about 1:4˜1:7. The manufacturing method may further include wrapping the exterior surface of the rolled first prepreg and second prepreg with an anti-resistant film, after rolling.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • The above and other objects, features and other advantages of the present invention will be more clearly understood from the following detailed description taken in conjunction with the accompanying drawings, in which:
  • FIG. 1 is an exemplary perspective view illustrating a hybrid piston pin in accordance with an exemplary embodiment of the present invention;
  • FIG. 2 is an exemplary cross-sectional view of the hybrid piston pin in accordance with an exemplary embodiment of the present invention;
  • FIG. 3 is an exemplary view illustrating when a first prepreg and a second prepreg are rolled and the exterior surface of the first prepreg is wrapped with a film in accordance with an exemplary embodiment of the present invention; and
  • FIG. 4 is an exemplary view illustrating when the first prepreg and the second prepreg are integrally molded in an oven in accordance with an exemplary embodiment of the present invention.
  • DETAILED DESCRIPTION
  • The present invention will be described more fully hereinafter with reference to the accompanying drawings, in which exemplary embodiments of the invention are shown. While the invention will be described in conjunction with exemplary embodiments, it will be understood that present description is not intended to limit the invention to those exemplary embodiments. On the contrary, the invention is intended to cover not only the exemplary embodiments, but also various alternatives, modifications, equivalents and other embodiments, which may be included within the spirit and scope of the invention as defined by the appended claims.
  • The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the singular forms “a”, “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises” and/or “comprising,” when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, components, and/or groups thereof. As used herein, the term “and/or” includes any and all combinations of one or more of the associated listed items. For example, in order to make the description of the present invention clear, unrelated parts are not shown and, the thicknesses of layers and regions are exaggerated for clarity. Further, when it is stated that a layer is “on” another layer or substrate, the layer may be directly on another layer or substrate or a third layer may be disposed therebetween.
  • Unless specifically stated or obvious from context, as used herein, the term “about” is understood as within a range of normal tolerance in the art, for example within 2 standard deviations of the mean. “About” can be understood as within 10%, 9%, 8%, 7%, 6%, 5%, 4%, 3%, 2%, 1%, 0.5%, 0.1%, 0.05%, or 0.01% of the stated value. Unless otherwise clear from the context, all numerical values provided herein are modified by the term “about.”
  • It is understood that the term “vehicle” or “vehicular” or other similar term as used herein is inclusive of motor vehicle in general such as passenger automobiles including sports utility vehicles (SUV), buses, trucks, various commercial vehicles, watercraft including a variety of boats, ships, aircraft, and the like and includes hybrid vehicles, electric vehicles, combustion, plug-in hybrid electric vehicles, hydrogen-powered vehicles and other alternative fuel vehicles (e.g. fuels derived from resources other than petroleum).
  • A hybrid piston pin in accordance with the present invention, as exemplarily shown in FIG. 1, may include a cylindrical pin 100 formed of steel, a first reinforcement layer 200 formed of a composite that includes reinforced fibers and a resin, having a cylindrical shape with a substantially uniform thickness and coupled to the interior surface of the cylindrical pin 100 and a second reinforcement layer 300 formed of a composite that includes reinforced fibers having an elasticity less than the reinforced fibers of the first reinforcement layer 200 and a resin, having a cylindrical shape with a uniform thickness and coupled to the interior surface of the first reinforcement layer 200.
  • A conventional piston pin is formed of SMC415 steel. Therefore, the conventional piston has a thickness of about 4.3 mm and a weight of about 79 g. The cylindrical pin 100 of the present invention may be formed of steel and in particular, may be formed of SMC415 steel. As will be described, reinforced materials may be coupled to the interior surface of the cylindrical pin 100 and the thickness of the cylindrical pin 100 may be reduced up to about 0.5-1.2 mm.
  • However, when the thickness of the cylindrical pin 100 is less than about 0.5 mm, flexural strength in a circular arrangement and flexural strength in a length direction may be diminished and thus, the cross-section of the cylindrical pin 100 may be deformed into an oval shape and the minimal thickness of the cylindrical pin 100 may not satisfy the required size tolerance. When the thickness of the cylindrical pin 100 exceeds about 1.2 mm, the hybrid piston pin of the present invention does not exhibit weight reduction effects as compared to the conventional piston pin formed of steel. Therefore, the thickness of the cylindrical pin 100 may be limited within the range of about 0.5-1.2 mm. The cylindrical pin 100 formed of steel may be disposed at the exterior most portion of the hybrid piston pin, may prevent thermal damage and may protect the reinforced materials. The exterior diameter of the cylindrical pin 100 may be within the range of about 7-9 mm.
  • The first reinforcement layer 200 may be rolled to have a cylindrical shape with a substantially uniform thickness and may be coupled to the interior surface of the cylindrical pin 100. The first reinforcement layer 200 may be formed of a composite that includes reinforced fibers and a resin. In particular, the first reinforcement layer 200 may be formed of a prepreg formed by pre-impregnating fibers with a resin. Thereafter, the second reinforcement layer 300 may be rolled to have a cylindrical shape with a substantially uniform thickness and may be coupled to the interior surface of the first reinforcement layer 200.
  • In other words, as referenced with respect to the first reinforcement layer 200, the second reinforcement layer 300 may be formed of a composite and may include reinforced fibers and a resin. For example, the second reinforcement layer 300 may be formed of a prepreg by pre-impregnating fibers with a resin. However, the reinforced fibers of the second reinforcement layer 300 may include a reduced elasticity as compared with the reinforced fibers of the first reinforcement layer 200. In particular, elasticity of the reinforced fibers of the second reinforcement layer 300 may be about one third or less that of the reinforced fibers of the first reinforcement layer 200. Therefore, the reinforced fibers that form the first reinforcement layer 200 and the second reinforcement layer 300 may be carbon fibers, the reinforced fibers of the first reinforcement layer 200 may be pitch-based carbon fibers, and the reinforced fibers of the second reinforcement layer 300 may be PAN-based carbon fibers.
  • Pitch-based carbon fibers, may have an elastic modulus of about 640 GPa or greater and may generally have an increased carbon content and an increased elasticity. Accordingly, the flexural strength and material strength of the hybrid piston pin in the circular arrangement when pitch-based carbon fibers may be coupled to the interior surface of the cylindrical pin 100 formed of steel. For example, the generation of deformation of the cylindrical pin 100 into an oval shape and bending deformation of the cylindrical pin 100 may be suppressed due to an applied load.
  • PAN-based carbon fibers, which have an elastic modulus of about 240 GPa or greater, may generally have an increased compressive strength. Further, the PAN-based carbon fibers may support the first reinforcement layer 200 and may withstand load when disposed at the interior most portion of the hybrid piston pin and the flexural strength of the hybrid piston pin in the circular arrangement may be increased. Accordingly, generation of deformation of the cylindrical pin 100 into an oval shape may be suppressed. PAN-based carbon fibers are relatively inexpensive and may reduce the cost. Further, as exemplarily shown in FIG. 2, the second reinforcement layer 300 may include a first composite layer 310 formed of reinforced fibers and a resin and may be disposed in parallel with the length direction of the cylindrical pin 100. Further, a second composite layer 320 formed of reinforced fibers and a resin and may be disposed perpendicular to the length direction of the cylindrical pin 100.
  • The reinforced fibers of the second reinforcement layer 300 are not limited to being disposed in one direction, for example, the reinforced fibers of the first composite layer 310 coupled to the interior surface of the first reinforcement layer 200 may be disposed in a direction parallel with the cylindrical pin 100 and the reinforced fibers of the second composite layer 320 coupled to the interior surface of the first composite layer 310 may be disposed in a direction perpendicular to the cylindrical pin 100. Accordingly, the stiffness of the hybrid piston pin may be improved and may withstand load applied in the width direction of the hybrid piston pin as well as load applied in the length direction of the hybrid piston pin.
  • Particularly, the first reinforcement layer 200 and the second reinforcement layer 300 may be integrally molded to increase a coupling degree of the first reinforcement layer 200 and the second reinforcement layer 300. Further, an adhesive film may be coupled to the exterior surface of the first reinforcement layer 200 to couple the first reinforcement layer 200 to the cylindrical pin 100 via the adhesive film. Moreover, when the reinforced fibers of the first reinforcement layer 200 are carbon fibers, potential corrosion may occur due to a potential difference between the carbon fibers and the cylindrical pin 100 formed of steel. The adhesive film may interrupt direct contact between the carbon fibers and the cylindrical pin 100 and may prevent potential corrosion to improve the durability of the hybrid piston pin.
  • By sequentially attaching the first reinforcement layer 200 formed of carbon fibers having relatively high elasticity and the second reinforcement layer 300 formed of carbon fibers having low elasticity to the interior surface of the cylindrical pin 100, the hybrid piston pin may have a weight of about 25-42 g and may achieve weight reduction by 46% or greater compared to conventional piston pins. Accordingly, when the hybrid piston pin of the present invention is applied to a vehicle, fuel efficiency of the vehicle may be improved by about 0.7-1.2%. Further, the hybrid piston pin of the present invention may have flexural strength in a circular arrangement of 57 MPa or greater and flexural strength in the length direction of 53 MPa and may satisfy desired material properties.
  • TABLE 1
    Flexural Flexural Flexural Flexural
    strength in strength in modulus in modulus in
    circular length circular length
    Configuration arrangement direction arrangement direction
    Test example 1 Including 70 MPa 60 MPa 109 GPa 81 GPa
    outer pitch-
    based
    reinforcement
    layer and
    inner PAN-
    based
    reinforcement
    layer
    Comparative Including 55 MPa 50 MPa 143 GPa 54 GPa
    example 1 single pitch-
    based
    reinforcement
    layer
    Comparative Including 170 MPa  50 MPa 103 GPa 36 GPa
    example 2 single PAN-
    based
    reinforcement
    layer
    Comparative Including 55 MPa 65 MPa 160 GPa 106 GPa 
    example 3 outer PAN-
    based
    reinforcement
    layer and
    inner pitch-
    based
    reinforcement
    layer
  • As shown from above Table 1, a hybrid piston pin in Test example 1 includes a first reinforcement layer 200 formed of pitch-based carbon fibers having relatively high elasticity and a second reinforcement layer 300 formed of PAN-based carbon fibers. The PAN-based carbon fiber has a relatively low elasticity and improved compressive strength and has flexural strength in a circular arrangement and flexural strength in the length direction, which are equal to or greater than those of a piston pin in Comparative example 1 that include a reinforcement layer formed of pitch-based carbon fibers.
  • Further, the hybrid piston pin in Test example 1 has improved flexural strength in the circular arrangement than a piston pin in Comparative example 2 and includes a reinforcement layer formed of PAN-based carbon fibers. The piston pin in Comparative example 2 has a flexural modulus less than the hybrid piston pin in Test example 1. The hybrid piston pin in Test example 1 has a greater flexural strength in the circular arrangement than a piston pin in Comparative example 3 that includes an exterior reinforcement layer formed of PAN-based carbon fibers and an interior reinforcement layer formed of pitch-based carbon fibers.
  • TABLE 2
    Thickness ratio Thickness ratio
    of cylindrical of cylindrical Flexural Flexural Flexural Flexural
    pin to first pin to second strength in strength in modulus modulus
    reinforcement reinforcement circular length in circular in length
    layer layer arrangement direction arrangement direction
    Test example 1:3 1:7 57 MPa 74 MPa 129 GPa 64 GPa
    2
    Test example 1:4 1:6 65 MPa 67 MPa 119 GPa 73 GPa
    3
    Test example 1:5 1:5 71 MPa 59 MPa 109 GPa 81 GPa
    4
    Test example 1:6 1:4 75 MPa 53 MPa 102 GPa 85 GPa
    5
    Comparative 1:2 1:7 41 MPa 70 MPa 131 GPa 44 GPa
    example 4
    Comparative 1:7 1:4 63 MPa 50 MPa 122 GPa 72 GPa
    example 5
    Comparative 1:6 1:3 72 MPa 48 MPa 102 GPa 82 GPa
    example 6
    Comparative 1:3 1:8 49 MPa 75 MPa 136 GPa 54 GPa
    example 7
  • As understood from above Table 2, as compared to hybrid piston pins in Text examples 2 to 5, a hybrid piston pin in Comparative example 4 has a thickness ratio of a cylindrical pin 100 to a first reinforcement layer 200 of less than 1:3 and has diminished flexural strength in the circular arrangement. A hybrid piston pin in Comparative example 5 has a thickness ratio of a cylindrical pin 100 to a first reinforcement layer 200 which exceeds a ratio of about 1:6 an has diminished flexural strength in the length direction.
  • Further, as compared to the hybrid piston pins in Text examples 2 to 5, a hybrid piston pin in Comparative example 6 has a thickness ratio of a cylindrical pin 100 to a second reinforcement layer 300 of less a ratio of about 1:4 and has reduced flexural strength in the length direction. In addition, a hybrid piston pin in Comparative example 7 has a thickness ratio of a cylindrical pin 100 to a second reinforcement layer 300 which exceeds a ratio of about 1:7 and has a reduced flexural strength in the circular arrangement.
  • A manufacturing method of a hybrid piston pin in accordance with the present invention includes stacking a first prepreg 10 that includes reinforced fibers and a resin and a second prepreg 20 that include reinforced fibers with a reduced elasticity as compared to the reinforced fibers of the first prepreg 10. A resin may be formed by rolling the first prepreg 10 and the second prepreg 20 to form the exterior surface of the first prepreg 10. The rolled first prepreg 10 and second prepreg 20 is integrally molded in an oven. In addition, the molded first prepreg 10 and second prepreg 20 is attached to the interior surface of a cylindrical pin 100 formed of steel.
  • As exemplarily shown in FIG. 3, the first prepreg 10 and the second prepreg 20 may be sequentially stacked in the upward direction and may then be rolled. For example, the stacked first prepreg 10 and second prepreg 20 may be rolled to form the exterior surface of the first prepreg 10 having relatively high elasticity. After rolling, the exterior surface of the rolled first prepreg 10 and second prepreg 20 may be wrapped with a film 30. As the film 30, a heat shrinkable tape having heat resistance may be employed.
  • Thereafter, as exemplarily shown in FIG. 4, the first prepreg 10 and second prepreg 20, wrapped with the film 30, may be placed into the oven and may be integrally molded. By wrapping the exterior surface of the rolled first prepreg 10 and second prepreg 20 with the film 30, the film 30 may shrink during heat exposure during molding within the oven and mesopores may be removed from the first prepreg 10 and second prepreg 20. When molding within the oven is completed, the film 30 may be removed and the molded first prepreg 10 and second prepreg 20 may be coupled to the interior surface of the cylindrical pin 100. Then processing may include cutting, surface grinding, etc., may be performed to complete manufacture of the hybrid piston pin.
  • In stacking, the reinforced fibers of the first prepreg 10 and the second prepreg 20 may be carbon fibers. In particular, the carbon fibers of the first prepreg 10 may be pitch-based carbon fibers, and the carbon fibers of the second prepreg 20 may be PAN-based carbon fibers and elasticity of the first prepreg 10 may be greater than elasticity of the second prepreg 20. Thereafter, the stacked first prepreg 10 and second prepreg 20 may be coupled to the interior surface of the cylindrical pin 100. A thickness ratio of the cylindrical pin 100 to the first prepreg 10 may be about 1:3˜1:6. Further, a thickness ratio of the cylindrical pin 100 to the second prepreg 20 to may be about 1:4˜1:7.
  • As is apparent from the above description, a hybrid piston pin in accordance with the present invention may be manufactured by sequentially stacking a reinforcement layer that includes reinforced fibers having high elasticity and a reinforcement layer that includes reinforced fibers having relatively low elasticity on the interior surface of a cylindrical pin formed of steel. Accordingly, the flexural strength in a circular arrangement may be increased and flexural strength in a length direction may be increased and a weight reduction by about 47˜67%, as compared to a conventional piston pin formed of steel may be achieved. Further, due to weight reduction, when the hybrid piston pin is applied to a vehicle fuel efficiency of the vehicle may be improved by about 0.7˜1.2% and costs may be reduced reduction.
  • Although the exemplary embodiments of the present invention have been disclosed for illustrative purposes, those skilled in the art will appreciate that various modifications, additions and substitutions are possible, without departing from the scope and spirit of the invention as disclosed in the accompanying claims.

Claims (10)

What is claimed is:
1. A hybrid piston pin, comprising:
a cylindrical pin formed of steel;
a first reinforcement layer formed of a composite including reinforced fibers and a resin, having a cylindrical shape with a uniform thickness, and coupled to the interior surface of the cylindrical pin; and
a second reinforcement layer formed of a composite including reinforced fibers, having, elasticity less than the reinforced fibers of the first reinforcement layer, and a resin, having a cylindrical shape with a uniform thickness, and coupled to the interior surface of the first reinforcement layer.
2. The hybrid piston pin according to claim 1, wherein the reinforced fibers of the first reinforcement layer and the second reinforcement layer are carbon fibers, wherein the reinforced fibers of the first reinforcement layer are pitch-based carbon fibers, and the reinforced fibers of the second reinforcement layer are PAN-based carbon fibers.
3. The hybrid piston pin according to claim 1, wherein a thickness ratio of the cylindrical pin to the first reinforcement layer is about 1:3-1:6.
4. The hybrid piston pin according to claim 3, wherein a thickness ratio of the cylindrical pin to the second reinforcement layer is about 1:4-1:7.
5. The hybrid piston pin according to claim 1, wherein the second reinforcement layer includes:
a first composite layer formed of reinforced fibers and a resin and disposed parallel to the length direction of the cylindrical pin; and
a second composite layer formed of reinforced fibers and a resin and disposed perpendicular to the length direction of the cylindrical pin.
6. The hybrid piston pin according to claim 1, further comprising: an adhesive film disposed between the cylindrical pin and the first reinforcement layer to couple the first reinforcement layer to the cylindrical pin.
7. A manufacturing method of a hybrid piston pin, comprising:
stacking a first prepreg including reinforced fibers and a resin and a second prepreg including reinforced fibers, having elasticity less than the reinforced fibers of the first prepreg, and a resin;
rolling the first prepreg and the second prepreg to form an exterior surface from the first prepreg;
integrally molding the rolled first prepreg and second prepreg in an oven; and
attaching the molded first prepreg and second prepreg to the interior surface of a cylindrical pin formed of steel.
8. The manufacturing method according to claim 7, wherein, in stacking of the first prepreg and the second prepreg, the reinforced fibers of the first prepreg and the second prepreg are carbon fibers, wherein the reinforced fibers of the first prepreg are pitch-based carbon fibers, and the reinforced fibers of the second prepreg are PAN-based carbon fibers.
9. The manufacturing method according to claim 8, wherein a thickness ratio of the cylindrical pin to the first prepreg is about 1:3˜1:6, and a thickness ratio of the cylindrical pin to the second prepreg is about 1:4˜1:7.
10. The manufacturing method according to claim 7, further comprising: wrapping the exterior surface of the rolled first prepreg and second prepreg with an anti-resistant film, after rolling.
US15/352,463 2016-04-25 2016-11-15 Hybrid piston pin and manufacturing method thereof Abandoned US20170307082A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
KR10-2016-0049898 2016-04-25
KR1020160049898A KR20170121752A (en) 2016-04-25 2016-04-25 Hybrid piston pin and manufacturing method of the same

Publications (1)

Publication Number Publication Date
US20170307082A1 true US20170307082A1 (en) 2017-10-26

Family

ID=60020888

Family Applications (1)

Application Number Title Priority Date Filing Date
US15/352,463 Abandoned US20170307082A1 (en) 2016-04-25 2016-11-15 Hybrid piston pin and manufacturing method thereof

Country Status (4)

Country Link
US (1) US20170307082A1 (en)
KR (1) KR20170121752A (en)
CN (1) CN107303739A (en)
DE (1) DE102016223462A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20190113138A1 (en) * 2017-10-18 2019-04-18 GM Global Technology Operations LLC Damper for piston and piston pin, for ice engines
US20210162487A1 (en) * 2019-09-25 2021-06-03 Shpac Co., Ltd Method of manufacturing hydraulic cylinder rod

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20190113138A1 (en) * 2017-10-18 2019-04-18 GM Global Technology Operations LLC Damper for piston and piston pin, for ice engines
US10393265B2 (en) * 2017-10-18 2019-08-27 GM Global Technology Operations LLC Damper for piston and piston pin, for ice engines
US20210162487A1 (en) * 2019-09-25 2021-06-03 Shpac Co., Ltd Method of manufacturing hydraulic cylinder rod

Also Published As

Publication number Publication date
KR20170121752A (en) 2017-11-03
CN107303739A (en) 2017-10-31
DE102016223462A1 (en) 2017-10-26

Similar Documents

Publication Publication Date Title
US20140352886A1 (en) Battery pack case assembly for electric and hybrid vehicles using a plastic composite and method for manufacturing the same
KR20160133605A (en) Reinforcement member for the auto part and the auto part comprising the same
US11333300B2 (en) High pressure tank
US20170307082A1 (en) Hybrid piston pin and manufacturing method thereof
KR20190111950A (en) Preform elements, and preforms using the same and methods for producing the same
KR101923381B1 (en) Composite material for reinforcement and articles comprising the same
KR101956131B1 (en) Composite material for reinforcement and articles comprising the same
US20130065469A1 (en) Large tow carbon fiber composite with improved flexural property and surface property
US20180105028A1 (en) Dog-Bone Type Rear Roll Rod
US20220314688A1 (en) Composite rim of vehicle wheel and method of manufacturing the same
CN106184083B (en) Bumper beam for vehicle
US8936844B2 (en) Composite chassis frame and method for manufacturing the same
US9796427B2 (en) Underbody structure for vehicle
US10406781B2 (en) Composite material with insert-molded attachment steel
US9022777B2 (en) Injection molding apparatus having an inner mold with a plurality of inner parts
US10384725B2 (en) Motor vehicle body assembly
US20190176589A1 (en) Hemming structure for hybrid-type door
US10828845B2 (en) Wire material for elastic member and elastic member
KR20130012871A (en) Method for manufacturing cross member of commerical automobile
KR101550296B1 (en) Manufacturing Method of Wheel Using Insulation Fiber Fabric and Wheel Manufactured by the Same
US20170297510A1 (en) Roof for vehicle
KR20180007020A (en) Composite piston pin and manufacturing method of the same
KR102239093B1 (en) Composite material for reinforcement and articles comprising the same
JP2016156464A (en) Brake hose
CN106864601B (en) Reinforcing member

Legal Events

Date Code Title Description
STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION